About: SNECMA 14R

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The SNECMA 14R was a 14-cylinder two-row air-cooled radial engine developed in France just prior to the start of World War II from the Gnome-Rhône 14N. The 14N radial engine was itself an improved version of the popular pre-war Gnome-Rhône 14K Mistral Major series; designed and manufactured by Gnome et Rhône, a major French aircraft engine manufacturer whose origins pre-date the First World War.

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  • The SNECMA 14R was a 14-cylinder two-row air-cooled radial engine developed in France just prior to the start of World War II from the Gnome-Rhône 14N. The 14N radial engine was itself an improved version of the popular pre-war Gnome-Rhône 14K Mistral Major series; designed and manufactured by Gnome et Rhône, a major French aircraft engine manufacturer whose origins pre-date the First World War. The improved 14R was initially known as the Gnome-Rhône 14P and then the Gnome-Rhône 14R. There were several improvements such as the introduction of a longer crankshaft and crankcase with a centre bearing, an increase in cylinder capacity, and a two-speed compressor. These changes allowed the engine to deliver 1,400hp at take-off and 1,300hp at 1,500m (1st gear) and 1200hp at 4000m (2nd gear). This came at the cost of a much increased total weight. It was expected that further development, such as the introduction of higher grade fuels, would lead to a power output of 1,660hp at low altitude. With the Fall of France, engine development was stopped under the occupation. After the war, development recommenced; however production of this engine after 1945 was transferred to the newly formed SNECMA and the engine was renamed the SNECMA 14R. (en)
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dbp:componentsOther
  • Starter: Air equipment electric inertia starter * Ignition: 2 x R.B. magnetos, 2 x short reach spark plugs per cylinder fed by a shielded ignition harness. (en)
dbp:compression
  • 6.800000 (xsd:double)
dbp:coolingsystem
  • Air-cooled with baffles (en)
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dbp:fuelsystem
  • 1 (xsd:integer)
dbp:fueltype
  • 92 (xsd:integer)
dbp:generalOther
  • Frontal Area: (en)
dbp:lists
  • * List of aircraft engines (en)
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dbp:oilcon
  • 0.006700 (xsd:double)
dbp:oilsystem
  • Pressure fed at (en)
dbp:performanceOther
  • 14 (xsd:integer)
dbp:power
  • *Take-off: at 2,600 rpm at Hg boost with 100 octane fuel **Military, low: at 2,600 rpm at **Military, high: at 2,600 rpm at **Normal, low: at 2,400 rpm at **Normal, high: at 2,400 rpm at (en)
dbp:power/weight
  • 1.494000 (xsd:double)
dbp:reductionGear
  • Planetary / epicyclic bevel reduction gearing at 0.67:1 ratio (en)
dbp:specfuelcon
  • 0.292000 (xsd:double)
dbp:specpower
  • 31.850000 (xsd:double)
dbp:supercharger
  • Gear-driven 2-speed supercharger at 6.5:1 and 9.0:1 ratios (en)
dbp:type
  • 14 (xsd:integer)
dbp:valvetrain
  • Single inlet and exhaust valves operated by rockers and pushrods (en)
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  • The SNECMA 14R was a 14-cylinder two-row air-cooled radial engine developed in France just prior to the start of World War II from the Gnome-Rhône 14N. The 14N radial engine was itself an improved version of the popular pre-war Gnome-Rhône 14K Mistral Major series; designed and manufactured by Gnome et Rhône, a major French aircraft engine manufacturer whose origins pre-date the First World War. (en)
rdfs:label
  • SNECMA 14R (en)
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